| 词条 | Scheibe SF 40 | |||||||||||||||
| 释义 |
The Scheibe SF 40 is a German two-seat ultralight aircraft designed and built by Scheibe Aircraft. DesignThe SF 40 is a two-seat low-wing ultralight monoplane with a fixed tricycle landing gear. It has a fabric-covered steel-tube fuselage with fabric-covered glass-fibre wings. The first SF 40 powered by a Sauer four-stroke engine flew in 1995 but after five were built it was replaced in 1997 by an improved variant, the SF 40C. The SF 40C is powered by a Rotax 912 engine with a two-bladed propellor, a shorter wing span than the original with increased fuel capacity. The SF 40C was awarded a type certificate in May 1998. Variants
Sauer-powered variant, five built.
Rotax 912-powered variant. Specifications (SF 40C){{aerospecs|ref= |met or eng?=met |genhide= |crew=2 |capacity= |length m= |length ft= |length in= |span m=9.50 |span ft=31 |span in=2 |height m= |height ft= |height in= |wing area sqm= |wing area sqft= |empty weight kg=287 |empty weight lb=633 |gross weight kg=450 |gross weight lb=992 |eng1 number=1 |eng1 type=Rotax 912 flat-four piston |eng1 kw=60 |eng1 hp=80 |eng2 number= |eng2 type= |perfhide= |max speed kmh=200 |max speed mph=124 |cruise speed kmh= |cruise speed mph= |stall speed kmh=53 |stall speed mph=39 |range km=700 |range miles=435 |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= }}{{aircontent |see also= |related= |similar aircraft= |sequence= |lists= }} References{{commons category|Scheibe Flugzeugbau}}
6 : German civil utility aircraft 1990–1999|Motor gliders|Scheibe aircraft|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1995 |
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